Nasa project final.ipynb
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Kernel status: Idle Executed 2 cellsElapsed time: 5 seconds
[1]:
!pip install requests
import requests
Requirement already satisfied: requests in c:\users\jones\anaconda3\lib\site-packages (2.32.3) Requirement already satisfied: charset-normalizer<4,>=2 in c:\users\jones\anaconda3\lib\site-packages (from requests) (3.3.2) Requirement already satisfied: idna<4,>=2.5 in c:\users\jones\anaconda3\lib\site-packages (from requests) (3.7) Requirement already satisfied: urllib3<3,>=1.21.1 in c:\users\jones\anaconda3\lib\site-packages (from requests) (2.2.3) Requirement already satisfied: certifi>=2017.4.17 in c:\users\jones\anaconda3\lib\site-packages (from requests) (2025.4.26)
[93]:
import pandas as pd
import requests
from datetime import datetime
[95]:
asteroids_data = [] #create an empty list
target = 10000
[97]:
API_KEY ="yQ53FWU1zfVKQvsXVVm4wEFe4XNxtOGYugMqQsxY"
[ ]:
url = f"https://api.nasa.gov/neo/rest/v1/feed?start_date=2024-01-01&end_date=2024-01-07&api_key={API_KEY}"
while len(asteroids_data) < target:
response = requests.get(url)
data = response.json()
details = data['near_earth_objects']
[ ]:
for date, ast_details in details.items():
for ast in ast_details:
asteroids_data.append(dict( #append values from the URL to the dictionary
id = int(ast['id']),
name = ast['name'],
absolute_magnitude_h = float(ast['absolute_magnitude_h']),
estimated_diameter_min_km = float(ast['estimated_diameter']['kilometers']['estimated_diameter_min']),
estimated_diameter_max_km = float(ast['estimated_diameter']['kilometers']['estimated_diameter_max']),
is_potentially_hazardous_asteroid = ast['is_potentially_hazardous_asteroid'],
neo_reference_id = int(ast['neo_reference_id']),
[ ]:
close_approach_date = ast['close_approach_data'][0]['close_approach_date'],
relative_velocity_kmph = float(ast['close_approach_data'][0]['relative_velocity']['kilometers_per_hour']),
astronomical = float(ast['close_approach_data'][0]['miss_distance']['astronomical']),
miss_distance_km = float(ast['close_approach_data'][0]['miss_distance']['kilometers']),
miss_distance_lunar = float(ast['close_approach_data'][0]['miss_distance']['lunar']),
orbiting_body = ast['close_approach_data'][0]['orbiting_body']))
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